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Rotax 582 Ul Engine 2-Piece Radiator Set (High Configuration) Parts

From $0.47 to $56.75
Reference Chart

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No. Rotax Part Number Description Qty Req PN Price Buy
8241-186 HEX.SCREW M6X162
15-00164
$0.47
Quantity
14951-870 CLAMP 16-254
15-03442
$5.85
Quantity
19866-710 CLAMP 142X2,5 MM2
15-01869
$1.18
Quantity
20956-260 LOW PRESSURE HOSE GC 7,5X12,5NBf
15-03520
$56.75
Quantity
23860-300 LOW PRESSURE HOSE GC 6X11NBf
15-01693
$56.75
Quantity
24951-898 CLAMP 7-112
15-03445
$8.50
Quantity
32841-580 HEX.SCREW M6X82
15-01194
$0.53
Quantity
Subtotal $0.00
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Overview

- Items not illustrated
  • a   cooling surface 3,2 dm2 (49,6 in2)
  • b   from engine S/N: 3,916.823
  • c   up to engine S/N: 4,916.822
  • d   for evacuation of air, at installation of engine with spark plugs down.
  • e   longer studs for 582 UL mod. 90 and 618 UL
  • f    in a roll.


Explanations of symbols and statements in part number charts:
  • N = Newly introduced part number
  • s.v. = Still valid. Part was replaced by compatible component and can not be supplied any longer by the producer. Existing stock may be used.
  • AR = As required. This generally refers to shims, hose, wires, and cable. Measure the amount you need before ordering. Many times there will be multiple listings of different lengths with the same part number. Use individual part descriptions to determine the proper length needed.
  • n.a or NLA = No longer available, no replacement from Rotax. Part is no longer available due to incompatibility to current production or unavailability of part.
  • CALL = Please call for price, 800-247-9653

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Please note, Aircraft Spruce Canada's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce Canada assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.